FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering and can be used for compartment separation. Aircraft compartment system comprises plug-in fastener, separator with pusher (two parallel pushers) with spherical thrust element. Said thrust element comprises circular bead with inner surface shaped to conical taper. Shaper geometrical centre is located at the centre of gravity of detachable compartment while thrust element hardness is higher than that pusher part in contact therewith.
EFFECT: accurate separation, lower power input for compartment stabilisation after separation and dynamic loads to detachable compartment.
6 cl, 2 dwg
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